Experimental laser sensing for aircraft vibration suppression

Ernest D. Shackelford, Anindya Ghoshal, Mannur Sundaresan, Mark J. Schulz, C. R. Ashokkumar, Frederick Ferguson

Research output: Contribution to journalArticlepeer-review

Abstract

The possibility of using a laser sensor and piezoelectric patches for vibration suppression on aircraft was demonstrated. The control technique significantly increased the damping ratio and reduced the steady-state vibration of a model wing in a low-speed wind tunnel. The performance could be improved by using actuators that have a large force and a filter with less phase lag. It was shown that the laser can operate in clouds, and darkness has no effect on laser.

Original languageEnglish
Pages (from-to)1394-1398
Number of pages5
JournalAIAA journal
Volume43
Issue number6
DOIs
StatePublished - Jun 2005

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